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IRIDIUM 8 (24792)
COSPAR: 1997-020A | Alt Name: Iridium 8
DECAYED
Image
Additional Sources
Launch Details
Launch Date
May 5, 1997
Launch Site
AFWTR
Launch Pad
SLC2W
Launch Vehicle
Delta 7920-10C
Orbital Elements
NORAD ID
24792
International Designator
1997-020A
Decay Date
11/24/2017
Basic Satellite Info
Name
IRIDIUM 8
Alternative Name
Iridium 8
Type
Payload
Status
Decayed
Owner
IRID
Country
United States
Constellation
N/A
Related Satellites
Major Events
N/A
Summary
IRIDIUM 8 is a communication satellite identified by NORAD CAT ID 24792 and OBJECT ID 1997-020A. Launched on May 5, 1997, from AFWTR (SLC2W) using the Delta 7920-10C launch vehicle, it is part of the LM700 bus configuration designed by MOTO/LMMS for the US-based Iridium constellation. The satellite has a box shape with two deployable solar panels and measures 3.5 meters in length and 1 meter in diameter, with a span of 5 meters. It had an initial launch mass of 662 kg and a dry mass of 556 kg, powered by solar arrays and batteries. The mission is focused on communication purposes, and its expected lifetime was 8 years.
Physical Characteristics
Length
3.5
Diameter
1
Span
5
Dry Mass
556
Launch Mass
662
Shape
Box + 2 Pan
Radar Cross Section
3.5089
Visual Magnitude
Unknown
Color
Unknown
Material Composition
Unknown
Technical Details
Payload
Iridium SV008
Purpose
Communication
Mission
Communication
Manufacturer
MOTO/LMMS
Life Expectancy
8 years
Bus
LM700
Configuration
LM-700A
Motor
?
Equipment
?
Power System
2 deployable solar arrays, batteries
ADCS
Unknown
Transmitter Frequency
Unknown
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